EFFECT OF NOSE BLUNTNESS AND CONE ANGLE ON SLENDER-VEHICLE TRANSITION - REPLY

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作者：

ERICSSON, LE

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AIAA JOURNAL | 1990年 / 28卷 / 07期

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V [航空、航天];

学科分类号：

08 ; 0825 ;

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页码：1338 / 1338

页数：1

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[1] EFFECT OF NOSE BLUNTNESS AND CONE ANGLE ON SLENDER-VEHICLE TRANSITION
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[2] Effect of nose bluntness and cone angle on slender-vehicle transition
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[3] EFFECT OF NOSE BLUNTNESS AND CONE ANGLE ON SLENDER-VEHICLE TRANSITION - COMMENT
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[4] PARAMETRIC INVESTIGATIONS OF SLENDER CONE NOSE BLUNTNESS EFFECTS
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[5] EFFECT ON SLENDER VEHICLE DYNAMICS OF CHANGE FROM SPHERICAL TO CONICAL NOSE BLUNTNESS
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[6] AERODYNAMICS OF A SLENDER CONE WITH ASYMMETRIC NOSE BLUNTNESS AT MACH-14
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[7] COMBINED EFFECTS OF NOSE BLUNTNESS AND CONE ANGLE ON UNSTEADY AERODYNAMICS
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[8] Effect of the Cone Nose Bluntness and the Ultrasonically Absorptive Coating on Transition in a Hypersonic Boundary Layer
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[9] Effect of the cone nose bluntness and the ultrasonically absorptive coating on transition in a hypersonic boundary layer
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[10] Effect of Nose Bluntness on Flowfield Over Slender Bodies in Hypersonic Flows
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